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The work in this paper deals with reconstructing and optimizing the wing geometry of an Unmanned Combat Aerial Vehicle for improved performance and reviewing the impact of the modification on flight parameters in a steady flight. The behavior of airfoils at planned flight conditions under I.S.A. is checked in XFLR5 software. Following up by 2-D CFD and boundary layer analysis of former and new airfoil, dimensions of the wing are re-developed, keeping the fuselage and tail structure same. The existing wing and the optimized wing design is analyzed by Vortex Lattice Method and Triangular Panel Method, with an objective to make the shape of the wing aerodynamically suitable for an increased Lift to Drag ratio and thereby minimizing drag coefficients.
Vishu Oza, Hardik Vala. 2021. "Airfoil Analysis and Effect of Wing Shape Optimization on Aerodynamic Parameters in a Steady Flight". Global Journal of Research in Engineering, Global Journal of Research in Engineering - D: Aerospace Science GJRE-D Volume 21 (GJRE Volume 21 Issue D1).
Crossref Journal DOI 10.17406/gjre
Print ISSN 0975-5861
e-ISSN 2249-4596
v1.2
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Total Score: 102
Country: India
Subject: Global Journal of Research in Engineering
Authors: Vishu K. Oza, Hardik R. Vala (PhD/Dr. count: 0)
View Count (all-time): 342
Total Views (Real + Logic): 861
Total Downloads (simulated): 71
Publish Date: 2021 01, Fri
Monthly Totals (Real + Logic):
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